JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5420' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5420' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA0600004Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285 AREA I/B STIFFENER AFTER FRAME CHORD REMOVAL. THE STIFFENER WAS REPLACED IAW ECRA 5420-01445.SDR UPS06146062Web · crackedINSPECTION TYPE:1C NR 2 PYLON LWR AFT OTBD MEMBRANE CRACKED. REMOVED AND REPLACED OB CRACKED WEB MEMBER ANGLE IAW SRM 51-40-00.SDR UPS06146061Web · crackedINSPECTION TYPE:1C NR 2 THE MOST AFT PYLON INBD MEMBRANE CRACKED. REMOVED AND REPLACED IB CRACKED WEB MEMBER ANGLE IAW SRM 51-40-00.SDR CALA0600014Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600013Stiffener · crackedINSPECTION FOUND A 4.5 INCH CRACK IN NR 1 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (STIFFENER) AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR CALA0600009Stiffener · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 PYLON I/B FRAME CHORD ATTACH SUPPORT -T- (SUPPORT STIFFENER) DURING FRAME CHORD REMOVAL AT NAC STA 285.45 TO NAC STA 295. THE SUPPORT STIFFENER WAS REPLACED IAW ECRA 5420-01444.SDR USAA051530Bracket · improperNR 2 PYLON NAC STA 144 IMPROPER FIT. INSTALLED NEWLY FABRICATED BRACKET PER EA 97148, DEFECT SIZE: 5.7 L X .7 W X .080 H INCH.SDR CA051208010Angle · crackedWHILE REPLACING THE ENGINE PYLON BOLTS AS PER THE SB601R-54-005, THE AME WORKING IN THE AREA NOTICED THAT BOTH THE LT AND RT SIDE FORMED ANGLES INSIDE ENGINE PYLON AT STA FS 640, STRINGER 10 WERE CRACKED. BOTH ANGLES P/N 601-37003-81 FOR THE LHS AND ANGLE P/NSDR DL76L050747Angle · crackedNR 1 ENGINE PYLON MID SPAR CLOSE OUT ANGLE WAS FOUND CRACKED. REPLACED CRACKED MID SPAR CLOSE OUT ANGLE AND INSPECTED MID SPAR FITTINGS, REF AD 2005-19-23.SDR DL76L050721Angle · crackedTHE NR 2 PYLON MID SPAR CLOSEOUT ANGLE WAS FOUND CRACKED. MID SPAR FITTING WAS INSPECTED AND CLOSEOUT ANGLE REPLACED PER ER/A 451663-14AD, REF AD 2005-19-23, 01-074944-12AD.SDR DL76L050720Angle · crackedTHE NR 1 PYLON MID SPAR FITTING CLOSEOUT ANGLES WAS FOUND CRACKED. THE MID SPAR FITTINGS WERE INSPECTED AND THE CLOSEOUT ANGLES WERE REPLACED, REF AD 2005-19-23, 01-074944-12AD.SDR DL76L050717Angle · crackedNR 2 PYLON CLOSEOUT ANGLE FOUND CRACKED. MID SPAR FITTING WAS INSPECTED FOR CRACKS AND CLOSEOUT ANGLE WAS REPLACED. REF AD 2005-19-23, 01-074944-12AD.SDR 05FDEA03824Support Angle · crackedNR 1 ENG NOSE COWL AFT SIDE LOWER SUPPORT WEB ANGLE FOR STARTER VALVE WAS CRACKED. REMOVED CRACK SUPPORT ANGLE FROM NR 1 ENGINE AFT SIDE OF AFT BULKHEAD NOSE COWL IAW DC10 SRM 51-31-01 VOL 11. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW DC10 SRM 51-31-01 VOL 1SDR QXEA200501522Cowl Door · crackedPDX: NR 2 ENGINE NACELLE COWL DOOR 422BL REQUIRES PERMANENT REPAIR OF FWD EDGE CRACKS. MAINTENANCE REPAIRED IAW QX EA 6-71-157, RD 8/4-71-097, QX EA 6-71-222, PSM 1-84-7A, 51-00-06 AND Q400 AMM TASK 51-25-31-370-801.SDR 05FDEA03750Bracket · crackedNR 1 PYLON FAIRING 475CL RT FWD BRACKET CRACKED.SDR 2005UALA01238Angle · crackedNR 1 PYLON MID SPAR AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER. NR 1 PYLON MID SPAR P/N 311T3157-1 AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER, VERIFIED WITH HFEC. THIS IS THE CLOSE-OSDR UPS05545735Web · crackedNR 1 PYLON SKIN CRACKED AT ACCESS PANEL 433AL CUTOUT NEAR 11:00 POSITION. REPAIRED CRACK ON NR 1 PYLON SKIN IAW GOODRICH ER NR 05-4594 AND IAW UPS EO B757-5430-23199-ASDR 0501916624Stiffener · crackedDURING "M" CHECK, FOUND CRACK IN INBOARD STIFFENER OF NR 4 PYLON AT NAC STA 217. REPAIRED PER EA 66-205836.SDR 05FDEA03414Bolt · shearedNR 1 PYLON, UPPER PLUG LOCKING BOLT HEAD SHEARED OFF DURING REMOVAL. REF BOLT P/N AUB7227-1. INSTALLED NR 1 PYLON UPPER PLUG LOCKING BOLT. REF M/M 54-00-01-4SDR 05FDEA03165Flange · crackedNR 1 PYLON FLANGE CRACKED BELOW COLD AIR DUCT.SDR 05FDEA03164Web · crackedNR 2 ENG LWR LT SIDE WEB 28" FROM NOSE COWL.SDR 05FDEA03163Web · crackedNR 2 PYLON LWR RT SIDEWEB CRACKED 28" FROM NOSE COWL.SDR CA050923008Vent · cracked(CAN) ON A SCHEDULED PHASE INSPECTION THIS VENT, WHICH IS ON THE ENGINE THRUST REVERSER COWL WAS FOUND TO HAVE A 2 INCH CRACK. A SIMILIAR CRACK WAS FOUND ON A PHASE CHECK THE DAY BEFORE ON ANOTHER AIRCRAFT.SDR CA050922004Panel · departed(CAN) WHEN DEPARTING, AC HAD A NR1 ENG NACELLE STRUT ACCESS PANEL DEPART FROM AC. AC WAS INSPECTED FOR DAMAGE RESULTING FROM DEPARTURE OF THIS PANEL, AND FOR POSSIBLE CAUSE. REST OF PANELS WERE CHECKED FOR SECURITY. NO ADDITIONAL FAULTS FOUND. AC WAS RELEASSDR UPS05145482Angle · crackedNR 1 PYLON LOWER AFT DOUBLER ANGLE CRACKED INBD SIDE. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON THE NR 1 PYLON IAW A300 SRM 51-40-00.SDR UPS05145481Angle · crackedNR 2 PYLON LOWER AFT DOUBLER ANGLE CRACKED. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON NR 2 PYLON IAW A300 SRM 51-40-00.SDR MALA050692Bushing · migratedWHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 3 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT.SDR MALA050693Bushing · migratedWHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 4 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT.SDR MALA050691Bushing · migratedWHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 2 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT.SDR MALA050690Bushing · migratedWHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND THE NR 1 ENGINE PYLON TO YOKE LINK BUSHINGS HAVE MIGRATED OUT.SDR UPS05245465Bushing · corrodedINSPECTION TYPE:C NR 1 ENGINE FWD ENGINE MOUNT PITTING CORROSION IN BORE OF MOUNT HOLES (TW O/B HOLES). BUSHINGS REPLACED IAW SOPM 20-50-03 AND EO B727-5440-1592 APNDX-A.SDR UIEA200500124Support · crackedD-CHECK, NR 2 PYLON, RT LWR AFT SKIRT FAIRING LOWER STIFFENER CRACKED. STOPPED DRILLED THE CRACK. NDT AND HFEC INSPECTED ALL AFFECTED FASTENER HOLES AND REPAIR AREA TO ENSURE CRACKS AND DAMAGE FREE CONDITION. FABRICATED AND INSTALLED 0.050 INCH THICK REPAIRSDR MALA050681Strap · chafedDURING 4K CHECK IN BNA REMOVED AND REPLACED RT NACELLE FIG 8 COWL ATTACH STRAP P/N 7254110-257 CHAFE DAMAGE. REMOVED AND REPLACED REF: EAMS WO 212753 TASK 4501 WORK ORDER SAAB SRM 51-40-22/21/25.SDR MALA050680Strap · chafedDURING 4K INSPECTION FOUND LT NACELLE FIG 8 INBOARD ATTACH CAM-LOCK STRAP CHAFED OUT OF LIMIT P/N 7254110-257. REMOVED AND REPLACED REF: EAMS WO 212753 TASK 4505 WORK REF: SAAB SRM 51-40-22/21/25.SDR MALA050647Cowl Door · chafedDURING INSPECTION, FOUND NR 4 AFT INBD COWL DOOR HAS CHAFING ON STIFFENER AT BOTTOM OF COWL DOOR.SDR MALA050644Cowl Door · chafedDURING INSPECTION FOUND NR 2 AFT OTBD COWL DOOR HAS CHAFING ON STIFFENER AT BOTTOM OF COWL DOOR.SDR MALA050643Cowl Door · damagedDURING INSPECTION FOUND DAMAGE TO STIFFENERS ON NR 1 AFT OTBD COWL DOOR CHAFFING ON STIFFENER AT BOTTOM OF COWL DOOR.SDR MALA050646Cowl Door · chafedDURING INSPECTION, FOUND NR 3 AFT INBD COWL DOOR HAS CHAFING ON STIFFENERS AT BOTTOM OF COWL DOOR.SDR MALA050645Cowl Door · chafedDURING INSPECTION, FOUND NR 3 AFT OTBD COWL DOOR HAS CHAFFING ON STIFFENER AT BOTTOM OF COWL DOOR.SDR 05FDEA02327Fairing · delaminatedNR 1 PYLON AFT FAIRING 473EL DELAMINATED.SDR 05FDEA02326Support Bracket · crackedNR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL.SDR 05FDEA02310Web · crackedNR 2 PYLON L/E AREA INSIDE PNL 421CL AFT HORIZONTAL WEB HAS CRACK.SDR 05FDEA02268Web · crackedCRACK 1.5 INCH PYLON NR 1 UPPER VERTICAL WEB AT STA YN268. REPAIR IAW 54-00-01 FIG 3 VOL I.SDR 05FDEA02267Web · crackedCRACK 1.5 INCH ON PYLON NR 1 UPPER VERTICAL WEB AT STA YN268. REPAIR IAW 54-00-01 FIG 3 VOL I.SDR 05FDEA02266Web · crackedCRACK 1 INCH LONG ON INTERNAL VERTICAL WEB AT STA YN298. REPAIR IAW SRM 54-00-01 FIG 3 VOL I.SDR UPS05445128Web · crackedINSPECTION TYPE:C NR 1 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD FRAME WEB (CRACK LENGTH 7/16"). NR 1 PYLON REAR MOUNT BULKHEAD FRAME WEB REPAIRED AS PER HX RS R54-53-35353 & UPS ENGINEERING FILE 747-54-20052, CONTINUE TO CONDUCT DETAIL VISUAL & HFEC INSPESDR ARWA20050907Structure · crackedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 2 PYLON FOOT STOOL INBOUND SIDE WITH CRACK, APPROXIMATELY 5/8".SDR ARWA20050905Structure · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL INBOUND SIDE WITH 1.750 INCH CRACK.SDR 05FDEA01713Seal · damagedCOMPLY WITH EA 8-5410-82094. NACELLES/PYLON-REPLACEMENT OF DAMAGED PYLON FAIRING SEAL. CLOSING ACTION ON 06/27/05, ON N/R S00083.COMPLIED WITH EA8-5410-82094.SDR UPS05144746Angle · crackedNR 1 AFT LOWER PYLON AT RIB 18 BOTH INBD AND OTBD SECTION MEMBERS ARE CRACKED ABOVE AND BELOW CNTR NUTPLATE. REMOVED AND REPLACED L-ANGLE MEMBERS IAW A300 SRM 51-40-00 AND 51-40-21.
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